View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57709U 26144.98799551 +.00000000 +00000-0 +52856-4 0 00001
2 57709 43.0077 46.8247 0001035 288.4630 71.6110 15.27573373 01
| Epoch (UTC): | 24 May 2026 23:42:42 |
| Eccentricity: | 0.0001035 |
| inclination: | 43.0077° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 46.8247° |
| argument of perigee: | 288.4630° |
| revolutions per day: | 15.27573373 |
| mean anomaly at epoch: | 71.6110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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